Method and system for determining height above ground using indirect information

• US 9,087,449 B1
• Filed: 05/13/2014
• Issued: 07/21/2015
• Est. Priority Date: 05/14/2013
• Status: Active Grant

• Current Assignee: Garmin International, Inc. (Garmin Limited)
• Original Assignee: Garmin International, Inc. (Garmin Limited)
• Inventors: Schueler, Kurt L., Munns, Anthony James, Parthasarathy, Bharath, Alfermann, Nathan J., Abi, Deebu K.
• Primary Examiner(s): Tweel, Jr., John A
• Application Number:
  US14/276,650
• Time in Patent Office: 434 Days
• Field of Search: 340/977, 340/970, 701/4, 701/120, 701/301
• US Class Current: 1/1
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32
• CPC Class Codes: G01C 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence
• CPC Class Codes: G08G 5/0004 Transmission of traffic-related information to or from an aircraft airborne radio transmission systems in general H04B7/185; airborne wireless networks H04W84/06
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0078 for monitoring traffic from the aircraft radar or analogous systems specially adapted for traffic control G01S13/91

Abstract

Techniques and systems are described that allow an air traffic display and/or avionics system of an aircraft to display and/or warn a pilot of aircraft targets for air traffic proximate to the aircraft or to suppress the display of on-ground air traffic targets. In some implementations, an integrated avionics system can use indirect information to determine whether an individual aircraft traffic target is to be presented to a pilot. For example, the integrated avionics system can determine whether an aircraft target is in proximity to the ground based on traffic tracking data corresponding to other aircraft.

Claims

1. A method of furnishing an air traffic display on an aircraft, the method comprising:

receiving Mode C transponder data from a first target aircraft, the received Mode C transponder data including pressure altitude information for the first target aircraft;

receiving traffic tracking data for a second target aircraft, the received traffic tracking data including pressure altitude information and an on-ground indication for the second target aircraft;

determining height above ground for the first target aircraft using the traffic tracking data from the second target aircraft; and

suppressing the display of the first target aircraft on the air traffic display based on the determined height above ground.

2. The method of claim 1, wherein the traffic tracking data includes Mode S transponder data, ADS-B data, or combinations thereof.

3. The method of claim 1, wherein the second target aircraft is the aircraft in which the air traffic display is located.

4. The method of claim 1, further including utilizing airport elevation information to determine the height above ground for the first target aircraft.

5. The method as recited in claim 1, wherein the received traffic tracking data additionally includes location information for the second target aircraft.

6. The method as recited in claim 5, wherein the location of the second target aircraft is compared to a location of the first target aircraft and the height above ground for the first target aircraft is determined using the difference between the pressure altitudes of the first and second target aircraft when the first target aircraft is in proximity to the second target aircraft and the on-ground indication indicates that the second target aircraft is on the ground.

7. The method as recited in claim 1, further comprising receiving Mode C transponder data from a plurality of target aircraft, determining the height above ground for each of the plurality of target aircraft using the traffic tracking data from the second target aircraft, and suppressing the display of the plurality of target aircraft based on the determined height above ground for each of the aircraft.

8. The method as recited in claim 1, wherein display of the first target aircraft is suppressed if the determined height above ground is near zero.

9. The method as recited in claim 1, further comprising;

receiving Mode C transponder data from a first plurality of target aircraft;

receiving traffic tracking data from a second plurality of target aircraft;

determining height above ground for each of the first plurality of target aircraft using the received traffic tracking data from one or more of the second plurality of target aircraft; and

suppressing the display of the first plurality of target aircraft based on the determined height above ground for each of the first plurality of target aircraft.

10. The method as recited in claim 1, wherein the height above ground for the first target aircraft is determined by the difference between the pressure altitudes for the first and second target aircraft when the on-ground indication for the second target aircraft indicates that the second target aircraft is on the ground.

11. An airborne air traffic display system comprising:

a receiver configured to receive Mode C transponder data from a first target aircraft and traffic tracking data for a second target aircraft, the Mode C transponder data including pressure altitude information for the first target aircraft and the traffic tracking data including pressure altitude information and an on-ground indication for the second target aircraft; and

a processor coupled with the receiver, the processor configured to—

determine height above ground for the first target aircraft using the traffic tracking data from the second target aircraft, and

suppress the display of the first target aircraft by the air traffic display based on the determined height above ground.

12. The system of claim 11, wherein the traffic tracking data includes Mode S transponder data, ADS-B data, or combinations thereof.

13. The system of claim 11, further including a memory coupled with the processor and configured to store airport altitude information, wherein the processor is configured to determine height above ground using the airport elevation information.

14. The system of claim 11, wherein the processor is configured to—

compare a location of the second target aircraft to a location of the first target aircraft, and

determine the height above ground for the first target aircraft using the difference between the pressure altitudes of the first and second target aircraft when the first target aircraft is in proximity to the second target aircraft and the on-ground indication indicates that the second target aircraft is on the ground.

15. The system of claim 11, wherein the receiver is configured to receive Mode C transponder data from a plurality of target aircraft and processor is configured to—

determine the height above ground for each of the plurality of target aircraft using the traffic tracking data from the second target aircraft, and

suppress the display of the plurality of target aircraft based on the determined height above ground for each of the aircraft.

16. The system of claim 11, wherein the processor determines the height above ground for the first target aircraft using the difference between the pressure altitudes for the first and second target aircraft when the on-ground indication for the second target aircraft indicates that the second target aircraft is on the ground.

17. The system of claim 11, further including a display operable to present a visual indication of the target aircraft such that the first target aircraft is not presented on the display when the first target aircraft is suppressed by the processor.

18. The system of claim 11, wherein the receiver includes a transponder for receiving the Mode C transponder data.

19. An airborne air traffic display system comprising:

a display;

a receiver configured to receive Mode C transponder data from a first target aircraft and Mode S transponder data for a second target aircraft, the Mode C transponder data including pressure altitude information for the first target aircraft and the Mode S transponder data including pressure altitude information and an on-ground indication for the second target aircraft; and

a processor coupled with the receiver and the display, the processor configured to—

determine height above ground for the first target aircraft using the Mode S transponder data from the second target aircraft; and

suppress the display of the first target aircraft by the display based on the determined height above ground.

20. The system of claim 19, wherein the processor determines the height above ground for the first target aircraft using the difference between the pressure altitudes for the first and second target aircraft when the on-ground indication for the second target aircraft indicates that the second target aircraft is on the ground.